Accession Number : AD0451011

Title :   WIND TUNNEL MEASUREMENTS OF THE AGARD CALIBRATION MODEL B AT TRANSONIC AND SUPERSONIC SPEEDS,

Corporate Author : NAVAL ORDNANCE LAB WHITE OAK MD

Personal Author(s) : Eades, James B., Jr.

Report Date : 14 SEP 1964

Pagination or Media Count : 24

Abstract : This report presents results of an investigation carried out in the Naval Ordnance Laboratory's Supersonic Tunnel Number 1 to determine the aerodynamic characteristics of the AGARD Calibration Model B. Tests were conducted at free-stream Mach numbers ranging from 0.70 to 3.50, at angles of attack from -4 to +10 degrees, over a Reynolds number range from 0.20 times 100to the 6th power to 0.62 times 10 to the 6th power. (Author)

Descriptors :   (*WIND TUNNEL MODELS, CALIBRATION), (*SUPERSONIC WIND TUNNELS, CALIBRATION), OGINES, CYLINDRICAL BODIES, SUBSONIC FLOW, TRANSONIC FLOW, SUPERSONIC FLOW, HEAT TRANSFER, PRESSURE, LIFT, PITCH (MOTION), TEST FACILITIES, MEASUREMENT, DELTA WINGS, TRANSONIC WIND TUNNELS.

Distribution Statement : APPROVED FOR PUBLIC RELEASE